N702AA
Registered owner: LANTECH LEASING LLC, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
30 reports on file, 1995-03-23 – 1999-07-26.
Part: CLAMPS — LOOSE (NR 3 ENGINE)
MIA - FLT 275 - AFTER TAKEOFF MIA EN ROUTE TO LRM, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. RESECURED LOOSE BLEED DUCT CLAMPS IN NR 3 ENGINE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOORBEAM — CORRODED (BS 380)
TUL - FOUND CORROSION ON FLOORBEAM, FS 380, RBL 50 1 INCH BY 4 INCH. CORROSION REMOVED AND PATCH INSTALLED TO REPLACE UPPER FLANGE OF FLOORBEAM PER SRM 53-10-8 FIG 3. (M)
Earlier reports · 1995–1998 · 28 reports
1998
Part: LIGHT — INOPERATIVE (CABIN)
TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ABOVE AFT DOOR AND IN VENTRAL STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY ABOVE AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRINGER — CORRODED (BS 490-495)
TUL - STR 490 - STR 495 AT STR 28R CORROSION ON SIDE OF STRINGER COMPLETE THROUGH STRINGER. FABRICATED STRINGER REPAIR SPLICE AND FILLER AND INSTALLED IAW SRM 53-10-3, FIG 1. TST: 47,528 HOURS. CYCLES: 24,511. (X)
Part: CLAMP — DEFECTIVE (NR 3 ENGINE)
DFW - FLT 919 - AFTER TAKEOFF DFW NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY CHECKLIST, RETARDED THROTTLE AND LIGHT EXTINGUISHED. DUMPED FUEL AND RETURNED TO LAND DFW WITHOUT INCIDENT. REMOVED AND REPLACED BOTH CLAMPS. RAN NR 3 ENGINE, NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: DUCT — RUPTURED (NR 3 ENGINE)
DFW - FLT 271 - AFTER TAKEOFF TUL DURING CLIMB-OUT, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. BLEED AIR SWITCH CLOSED AND THROTTLE RETARDED TO IDLE PER EMERGENCY PROCEDURES. AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RUPTURED DUCT AND ACCOMPLISHED REQUIRED CHECKS PER MM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M)
Part: DUCT — RUPTURED (AFT FUSELAGE)
ORD - FLT 1966 - AFTER TAKEOFF ORD, FLIGHT CREW TURNED ON WING ANTI-ICE AND HEARD A LOUD BANG FOLLOWED BY VIBRATION. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. CHECK OF AIRCRAFT REVEALED TWO SUPPLY DUCTS RUPTURED. AIRCRAFT MAINTENANCE REPLACED RUPTURED SUPPLY DUCTS AND AS A PRECAUTION, REPLACED ENGINE BLEED AIR SHUT-OFF VALVE. SYSTEM GROUND AND LEAKED CHECKED NORMAL OPERATION. (X)
1997
Part: HARNESS — BROKEN (NLG)
DFW - FLT 0635 - DURING APPROACH TO DFW AFTER LANDING GEAR EXTENDED, NOSE LANDING GEAR INDICATION CHANGED FROM GREEN TO RED. RECYCLED LANDING GEAR WITH SAME RESULTS. VISUALLY CONFIRMED NLG DOWN AND LOCKED AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT NLG DOWNLOCK SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — DEFECTIVE (AFT STAIRS)
DFW - DURING OVERNIGHT CHECK, AFT VENTRAL STAIRWAY EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT VENTRAL STAIRWAY EMERGENCY EXIT LGIHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: STIFFENER — CORRODED (BS 590)
TUL - FOUND SUPPORT (STIFFENER) BEHIND SIL PLATE HAS SURFACE CORROSION. REPLACED SUPPORT STIFFENER WITH NEW STIFFENER PER SRM 51-10-1. (M)
Part: CASTING — CORRODED (BS 606-610)
TUL - FOUND ALUMINUM CASTING AND WEB BEHIND SIL PLATE HAS CORROSION. REPLACED WEB AND CASTING WITH NEW WEB AND CASTING PER SRM 51-10-1. (M)
Part: STRINGER — CORRODED (BS 1177-1180)
TUL - FOUND CORROSION INSIDE STRINGER 30, STATION 1177-1180. REPLACED STRINGER BRACKET INSIDE STRINGER 30 WITH NEW PART, TREATED AND PAINTED, SRM 51-10-2. (M)
Part: STRINGER — CORRODED (BS 950-970)
TUL - FOUND STRINGER 29R CORRODED AT BELL FRAMES FROM STATION 950 TO 970. REPLACED STRINGER 29R, INSTALLED SKIN DOUBLER PER SB 727-53-0179. STRINGER REPLACED FROM 950 TO 1005. (M)
Part: SKIN — CORRODED (BS 720)
TUL - FOUND FUSELAGE SKIN CORROSION ON ACCESS DOOR LANDING. REMOVED CORROSION, FABRICATED AND INSTALLED SHIM, TREATED AND PRIMED PER ESO 11697 DATED 4-2-06. (M)
Part: SUPPORT — CORRODED (BS 1172-1181)
TUL - CORROSION ON LOWER LAVATORY PAN SUPPORT ABOVE STR 221, STA 1172 TO STA 1176. CORROSION ON LAVATORY PAN, STA 1179 AFT OF WATER HOSE CONNECTION JUST BELOW STR 21L. REMOVED CORRODED LAVATORY PAN AND SUPPORT. INSTALLED NEW LAVATORY PAN AND SUPPORT HOSE FITTINGS AND PUMP VALVE PER SRM 51-10-1. TST: 42,325 HRS. CYCLES, 22,016. (X)
Part: SILL PLATE — CORRODED (BS 568-572)
TUL - CORROSION ON SILL PLATE WEB ON FORWARD CARGO DOOR AND CASTING. REPLACED SILL AND CASTING WITH NEW PARTS PER SRM 51-10-1, PAGE 4. TST: 42,325 HRS. CYCLES, 22,016. (X)
Part: FLOOR PAN — CORRODED (BS 1177)
TUL - CORROSION 1 INCH BELOW FLOORBOARD, STA 1177, LBL 12 INCHES TO 16 INCHES, IN AFT CARGO. REMOVED FLOOR WEB AND INSTALLED NEW FLOOR WEB PER SRM 51-30-2, SRM 51-20-4. TST: 42,325 HRS. CYCLES, 22,016. (X)
Part: SKIN — CORRODED (BS 581)
TUL - FOUND CORROSION BELLY SKIN ABOVE STRINGER 27L, STATION 581. REMOVED CORROSION OUT OF LIMITS. CUT OUT AFFECTED AREA AND INSTALLED EXTERIOR REPAIR ON SKIN IAW SRM 53-30-3 AND SRM 51-10-6. (M)
Part: STRINGER — CORRODED (BS 875-685)
TUL - FOUND CORROSION IN INSIDE CHANNEL OF STRINGER IN BOTTOM. CUT OUT DAMAGED AREA OF STRINGER SPLICED IN NEW SECTION PER SRM 51-10-1. (M)
Part: SHEAR TIE — CORRODED (BS 580)
TUL - FOUND SHEAR TIE HAS CORROSION, STATION 580, BETWEEN STRINGER 26L AND 27L. REMOVED AND REPLACED SHEAR TIE. (M)
Part: FLOOR BEAM — CORRODED (BS 1130)
TUL - FOUND STATION 1130 FLOORBEAM LOWER SIDE HAS CORROSION UNDER NUT PLATES BL 5R TO 36L, AFTER NUT PLATE AND CUSHION TAPE REMOVED. COMPLETED REPAIR PER EOS 11697 DATED 4-17-96. (M)
Part: ANGLE — CORRODED (BS 380-384)
TUL - FOUND CREASE ANGLE CORRODED AROUND DRAIN HOLE, RIGHT FORWARD SERVICE DOOR, SILL. REMOVED AND REPLACED CREASE ANGLE, PER AARD 51-20-01-1. (M)
Part: STRINGER — CORRODED (BS 740)
TUL - FOUND CORROSION ON INBOARD SIDE OF STRINGER 27R CHANNEL AT 740 BULKHEAD FITTING. CUT OUT AND REMOVED DAMAGE SECTION OF STRINGER. INSTALLED STRINGER SPLICE AS PER SRM 53-10-3 FIG 1. (M)
Part: STRINGER — CORRODED (BS 626)
TUL - FOUND 6 INCHES OF 27R STRINGER REMOVED OF CORROSION, STATION 626. REMOVED CORRODED STRINGER 10 INCH PART, INSTALLED TWO PARTS OF STRINGER ON EACH SIDE OF FLOOR FRAME STATION 620, FORWARD CARGO. (M)
Part: FITTING — CORRODED (BS 950)
TUL - FOUND STATION 950 BUTT SPLICE CORRODED BETWEEN STRINGER 28-29R, AFT CARGO. REPLACED T-FITTING PER SRM 51-10-1. (M)
Part: FRAME — CORRODED (BS 985)
TUL - FOUND BELL FRAME CORRODED WITH DEEP PITTING. INSTALLED REPLACEMENT BELL FRAME AT STATION 985, BETWEEN STRINGER 29RT TO 30RT. (M)
Part: ANGLE — CRACKED (BS 804.5)
TUL - CRACK IN CHORD ANGLE AT FASTENER HOLE BS 804.5, STRINGER 14R. STOP DRILLED CRACKS PER SRM 51-10-1, INSTALLED DOUBLER PER SRM 51-40-3. (M)
Part: ANGLE — CRACKED (BS 804.5)
TUL - FOUND CRACK IN CHORD ANGLE AT FASTENER HOLE BS 804.5, STRINGER 14L. STOP DRILLED CRACK PER SRM 51-10-1, INSTALLED DOUBLER PER SRM 51-40-3. (M)
Part: SEAT TRACK — CRACKED (BS 458-460)
TUL - STATION 458 TO 460, RIGHT INBOARD SEAT TRACK HAS CRACK AND CORRSION INSIDE CHANNEL FOR FEET LOCK DOWNS. INSTALLED NEW SEAT TRACK FROM STAITON 440 TO 480 AS PER SRM 53-10-5. (M)
1995
Part: SLIDE — FAILED (PAX DOOR)
ORD - DURING SHOP TEST INFLATION, EMERGENCY EVACUATION SLIDE SEAM FAILED, SCRAPPED EMERGENCY EVACUATION SLIDE. (Z)